# N917FD: Boeing 757-23A - Status: Valid registration - Airframe: [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a) (registry code 1384967, 178 seats) - Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (The Boeing Company) (OpenAirDocs) - Serial number: 24291 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: August 20, 2008 - Expires: February 29, 2028 - Mode S code: ACB12D - Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=917FD - Page: https://openairdocs.org/aircraft/N917FD From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Boeing 757-23A) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N917FD. ## FAA accident and incident reports None matched to N917FD. ## Service difficulty reports (195, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA202608211211](https://openairdocs.org/sdr/FDEA202608211211), Aug 21, 2026: POWER SUPPLY. FAULTED. R1 EMERGENCY EXIT LIGHT FAILS OPS TEST. PREMATURE REMOVAL/INSTALLATION OFF MPN: 2012-1. REPLACED BATTERY, NO HELP. REMOVED AND REPLACED POWER SUPPLY/TRAY ASSY A - [SDR FDEA202607100886](https://openairdocs.org/sdr/FDEA202607100886), Jul 10, 2026: LANYARD. OUT OF POSITION. DURING PREFIGHT FOUND R-1 DOOR WILL NOT ARM . DOOR IS LOCKED AND INDICATED. AMM: 25-66-01-4 FOUND R1 PASSENDER DOOR STATIC LINE CAUGHT IN PUSHROD. REROUTED CARB - [SDR FDEA202604030397](https://openairdocs.org/sdr/FDEA202604030397), Apr 3, 2026: SKIN. DENTED. R/WING O/B T/E MAIN FLAP LOWER SURFACE HAS A DENT PANEL ASSY SKIN OUTER PLY THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5750-T0386919. - [SDR FDEA202604020393](https://openairdocs.org/sdr/FDEA202604020393), Apr 2, 2026: FRAME. CRACKED. DURING ACCOMPLISHMENT WC EF 530-E0329085 D P6 MAIN FRAME BODY STATION 1640 FUSELAGE FRAME INSPECTION FOUND MISSING INTERNAL STRAP IN FRAME AT BS 640 BETWEEN STR - [SDR FDEA202602110171](https://openairdocs.org/sdr/FDEA202602110171), Feb 11, 2026: FLEX LINE. LEAKING. ON APPROACH EXTENDING MLG & FLAPS TO 20, LT HYD QTY EICAS & COMPLETE LOSS OF LT SYS HYD FLUID. MAINTAINED CONFIGURATION & COMPLETED LT HYD QTY QRH PROCEDURE PRI - [SDR FDEA202406230855](https://openairdocs.org/sdr/FDEA202406230855), Jun 23, 2024: BATTERY PACK. FAILED. DURING SVC FOUND THE L1 INSIDE AND OUT EMERGENCY LIGHTS WERE INOP. REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK AS REQUIRED IAW AMM 33-51-07-2. OPS - [SDR FDEA202403220346](https://openairdocs.org/sdr/FDEA202403220346), Mar 22, 2024: HINGE FITTING. CRACKED. DURING ROTO INSPECTION OF LH STA 1640 S-14L. A CRACK INDICATION WAS NOTED IN OUTBD UPPER HOLE AT 2 O'CLOCK (VIEW LOOKING AFT) REMOVED AND REPLACED WITH NEW HING - [SDR FDEA202403210338](https://openairdocs.org/sdr/FDEA202403210338), Mar 21, 2024: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD PANEL 232MJF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MJF ON VT MAE TRAVELER T24/1738386 IAW DWG SRZ-25-005 REVISION "R" MAJOR REP - [SDR FDEA202403210332](https://openairdocs.org/sdr/FDEA202403210332), Mar 21, 2024: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD PANEL 252MUF BROKEN. FABRICATED ZONE 250 FLOORBOARD PANEL 252MUF ON VT MAE TRAVELER T24/1738390 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPA - [SDR FDEA202403210331](https://openairdocs.org/sdr/FDEA202403210331), Mar 21, 2024: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD PANEL 251MUF DAMAGED. FABRICATED ZONE 250, 251MUF FLOORBOARD PANEL ON VT MAE TRAVELER T24/1738388 IAW DWG SRZ 25-005 REV "R" MAJOR REPAIR - [SDR FDEA202403140289](https://openairdocs.org/sdr/FDEA202403140289), Mar 14, 2024: FLOOR PANEL. DAMAGED. MAIN CABIN FLOORBOARD PANEL 231MEF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 231MEF ON VT MAE TRAVELER # T24/1738374 IAW DWG SRZ-25-005 REVISION R MAJOR REP - [SDR FDEA202403140288](https://openairdocs.org/sdr/FDEA202403140288), Mar 14, 2024: FLOOR PANEL. DAMAGED. MAIN DECK FLOORBOARD PANEL 231MFF DAMAGED FABRICATED ZONE 230 FLOORBOARD PANEL 231MFF ON VT MAE TRAVELER # T24/1738381 IAW DWG SRZ-25-005 REVISION R MAJOR REPAI - [SDR FDEA202403140287](https://openairdocs.org/sdr/FDEA202403140287), Mar 14, 2024: FLOOR PANEL. DAMAGED. ZONE 220 COURRIER FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221BF ON VT MAE TRAVELER # T24/1738060 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR - [SDR FDEA202403140286](https://openairdocs.org/sdr/FDEA202403140286), Mar 14, 2024: FLOOR PANEL. DAMAGED. ZONE 220 COURIER FLOORBOARD 221MBF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 221MBF ON VT MAE TRAVELER # T24/1738161 IAW DWG SRZ-25-005 REVISION R MAJOR RE - [SDR FDEA202403140285](https://openairdocs.org/sdr/FDEA202403140285), Mar 14, 2024: FLOOR PANEL. DAMAGED. ZONE 220 COURIER FLOORBOARD 222MAF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222MAF ON VT MAE TRAVELER # T24/1738162 IAW DRAWING SRZ-25-005 REVISION R MAJO - [SDR FDEA202309231639](https://openairdocs.org/sdr/FDEA202309231639), Sep 23, 2023: CONTROLLER. FAILED. LOST CABIN PRESSURE DESCENDING THROUGH APPROX FL 280. RECEIVED CABIN ALTITUDE WARNING MESSAGE. CABIN ALTITUDE SHOWED 10,000 & CLIMBING AT 500 FT/MIN. EMERGENCY - [SDR FDEA202305090834](https://openairdocs.org/sdr/FDEA202305090834), May 9, 2023: MICROPHONE. FAULTED. LEFT RADIO TRANSMITS INTERMITTENTLY. WHEN ATC IS ABLE TO HEAR THE TRANSMISSION THEY REPORT ONLY BEING ABLE TO HEAR 3 BY 5. A LOUD STATIC ACCOMPANIES EVERY TRANS - [SDR FDEA202212263019](https://openairdocs.org/sdr/FDEA202212263019), Dec 26, 2022: METERING VALVE. FAILED. RT HYD QTY EICAS MESSAGE IN FLIGHT, FOLLOWED BY RT HYD ENGINE PUMP EICAS MESSAGE, FOLLOWED BY RT HYD SYS PRESS MESSAGE. EMERGENCY DECLARED. CHECKED BOTH ANTI-SK - [SDR FDEA202209052207](https://openairdocs.org/sdr/FDEA202209052207), Sep 5, 2022: SOCKET. FAILED. AT BLOCK IN THE SLIDE ARM LIGHT ON DOOR L1 IS BURNT OUT. SERVICED L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT WITH NEW BULB WITH NO HELP. TRIED WITH THE LENS & BU - [SDR FDEA202205181242](https://openairdocs.org/sdr/FDEA202205181242), May 18, 2022: FLOOR PANEL. DAMAGED. FOUND DAMAGE ON FLOOR PANEL AT POS. 11RON STA 1300 RBL 55.00 SEE JOBCDID ON 53211717 PERFORMED PERMANENT REPAIR PER SRM 53-00-50-2R, PARAGRAPH 3.C,FIG/ 201. REV - [SDR FDEA202205031336](https://openairdocs.org/sdr/FDEA202205031336), May 3, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK RBL 24 BETWEEN STA 1520-1540 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52, FIG.201 REPAIR 1 - [SDR FDEA202204261333](https://openairdocs.org/sdr/FDEA202204261333), Apr 26, 2022: NONE. NONE. SUSPECTED REPAIR/SPLICE OUTER CREASE BEAM R/H STA 1400-1420 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.O # F-5310-T0368544, CREASE BEAM OUTBOARD CHORD, STA 14 - [SDR FDEA202204261326](https://openairdocs.org/sdr/FDEA202204261326), Apr 26, 2022: NONE. NONE. UNDOCUMENTED EXISTING REPAIR ON L/H WING INBD FLAP OUTBD TRAILING EDGE LWR SKIN ADJACENT NO 5 SPOILER PERFORMED WORK STEPS PER EA 000710. MAJOR REPAIR. - [SDR FDEA202204261325](https://openairdocs.org/sdr/FDEA202204261325), Apr 26, 2022: NONE. NONE. UNDOCUMENTED EXISTING REPAIR ON L/H WING INBD MAIN FLAP LWR SKIN APPROX WS 231.5 PERFORMED WORK STEPS PER EA 000711 - [SDR FDEA202204261302](https://openairdocs.org/sdr/FDEA202204261302), Apr 26, 2022: NONE. NONE. UNDOCUMENTED EXISTING REOAIR/SPLICE AT AFT CARGO STA 1540-1560 RBL 13 THIS REPAIR COMPLY WITH SRM 53-60-53-2R, NO DAMAGE OR DEVIATIONS NOTED, AND PERFORMED REPA - [SDR FDEA202204261301](https://openairdocs.org/sdr/FDEA202204261301), Apr 26, 2022: NONE. NONE. SUSPECTED REPAIR ON APU FIREWALL AT STA 1885.2 UPPER PART (APU SUPPORT STRUT L/H SIDE) THE REPAIR COMPLY WITH SRM 53-80-08-2R, NO DAMAGE OR DEVIATION NOTED, AND - [SDR FDEA202204261300](https://openairdocs.org/sdr/FDEA202204261300), Apr 26, 2022: NONE. NONE. UNDOCUMENTED EXISTING REPAIR ON APU FIRE WALL AT STA 1885.2 LWR PART THIS REPAIR COMPLY WITH SRM 53-80-08-2R, AND NO DAMAGE OR DEVIATIONS NOTED, AND REPAIR ASSE - [SDR FDEA202204261238](https://openairdocs.org/sdr/FDEA202204261238), Apr 26, 2022: SKIN. DENTED. FOUND DENT ON ELEVATOR R/H SIDE LWR SKIN , SIZE : D=0.0130" L=0.839" W=0.691" PERFORMED REPAIR PER SRM 51-70-17,REF. SRM 55-20-01-2R,FIG. 201,TABLE I.REV. 135.0 - [SDR FDEA202204261233](https://openairdocs.org/sdr/FDEA202204261233), Apr 26, 2022: SKIN. DENTED. FOUND DENT ON HORIZONTAL STABILAIZER R/H SIDE LWR SKIN , SIZE : D=0.0231" L=2.79" W=2.46" PERFORMED HOT BOND REPAIR PER SRM 51-70-10,REPAIR 4,REF. SRM 55-10-01- - [SDR FDEA202204261232](https://openairdocs.org/sdr/FDEA202204261232), Apr 26, 2022: SKIN. NONE. UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 LBL 7" DIMENSION 4.5"-5.0" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND E - [SDR FDEA202204261231](https://openairdocs.org/sdr/FDEA202204261231), Apr 26, 2022: SKIN. NONE. UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 LBL 16.5" DIMENSION 4.0"-4.3" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUN - [SDR FDEA202204261230](https://openairdocs.org/sdr/FDEA202204261230), Apr 26, 2022: SKIN. NONE. UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 RBL 16.5" DIMENSION 4.3"-4.2" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUN - [SDR FDEA202204251338](https://openairdocs.org/sdr/FDEA202204251338), Apr 25, 2022: SEAT TRACK. CORRODED. CABIN BETWEEN STA 560-580 FOUND CORROSION ON SEAT TRACK RBL 24.7 PERFORMED SEAT TRACK REAPAIR PER SRM 53-00-52 2R, FIG.201 REPAIR 1 MAJOR REPAIR - [SDR FDEA202204251337](https://openairdocs.org/sdr/FDEA202204251337), Apr 25, 2022: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1340-1380 FOUND SEVERAL CORROSION ON SEAT TRACK RBL 24.75 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52. FIG.201, REPAIR 1 - [SDR FDEA202204251335](https://openairdocs.org/sdr/FDEA202204251335), Apr 25, 2022: SEAT TRACK. CORRODED. CABIN STA 660 FOUND CORROSION ON SEAT TRACK LBL 58.22 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52 2R, FIG.201 REPAIR 1 MAJOR REPAIR - [SDR FDEA202204251334](https://openairdocs.org/sdr/FDEA202204251334), Apr 25, 2022: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1320-1360 FOUND SEVERAL CORROSION ON SEAT TRACK RBL 45.5 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52.FIG.201 REPAIR 1 - [SDR FDEA202204251332](https://openairdocs.org/sdr/FDEA202204251332), Apr 25, 2022: SEAT TRACK. DAMAGED. CABIN BETWEEN STA 560-580 FOUND ELONGATED HOLE BL 0 WORK ACCOMPLISHED PER FEDEX E.A # F-5310-T0368383, ELONGATED HOLE AT HORIZONTAL FLANGE OF SEAT TRACK AT BS 0 - [SDR FDEA202204251331](https://openairdocs.org/sdr/FDEA202204251331), Apr 25, 2022: SEAT TRACK. GOUGED. CABIN STA 582 FOUND DEEP GOUGE/CHAP MARK AT SEAT TRACK LBL45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368307, STA 440-680, LBL 45.5, SEAT TRACK - [SDR FDEA202204251330](https://openairdocs.org/sdr/FDEA202204251330), Apr 25, 2022: NONE. NONE. CABIN STA 680 FOUND CORROSION ON BEAM EXISTING REPAIR LBL22-RBL12 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368538, SECTION 43, FLOOR BEAM ASSY, - [SDR FDEA202204251329](https://openairdocs.org/sdr/FDEA202204251329), Apr 25, 2022: FLOORBEAM. CORRODED. CABIN BETWEEN STA 1200 FOUND CORROSION ON BEAM BETWEEN RBL 3-RBL 19 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368550: SECTION 45, FLOOR BEAM ASS - [SDR FDEA202204251306](https://openairdocs.org/sdr/FDEA202204251306), Apr 25, 2022: SEAT TRACK. DAMAGED. CABIN BETWEEN STA 1200-1240 FOUND 2 PLACES WONGATED HOLES ON SEAT TRACK RBL 24.75 DAMAGED SEAT TRACK REMOVED AND NEW SEAT TRACK INSTALLED PER SRM 53-00-52-2R, R - [SDR FDEA202204251305](https://openairdocs.org/sdr/FDEA202204251305), Apr 25, 2022: STRAP. CORRODED. CABIN STA 1420 FOUND CORROSION ON INTERCOSTAL STRAP RBL 24.75 AND RBL 45.5 PERFORMED FLOOR BEAM REPAIR STABILIZATION STRAP PER SRM 53-00-51-2R, FIG.201 REPAIR 1 - [SDR FDEA202204201241](https://openairdocs.org/sdr/FDEA202204201241), Apr 20, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL P.N 118662181-19 AT STA 680 NIR CARGO DOOR FOUND BROKEN PERFORMED WET LAYUP REPAIR FOR MENTIONED FLOOR PANEL PER SRM 53-00-50-2R, PARAGRAFH 3.D, FIG - [SDR FDEA202204191251](https://openairdocs.org/sdr/FDEA202204191251), Apr 19, 2022: TORQUE RING. CHAFED. ENG NO 2 OUTBORD C-DUCT ON THE UPPER FWO SIDE THERE IS A BROKEN PIECE FROM THER PANEL PERFORMED REPAIR PER SRM 51-71-03, REF. SRM 54-30-70-2R, FIG. 201,DETAIL I - [SDR FDEA202204191239](https://openairdocs.org/sdr/FDEA202204191239), Apr 19, 2022: PANEL. CRACKED. PYLON NO 2 THERE IS A CRACK ON PANEL NO 444DR FEO SIDE PERFORMED HOT BOND REPAIR PER SRM 51-70-04,REF. SRM 54-50-70-2R,FIG. 201,DETAIL I,TABLE I.REP. DIM.: 2,5" - [SDR FDEA202204191168](https://openairdocs.org/sdr/FDEA202204191168), Apr 19, 2022: FLOOR PANEL. BROKEN. FLOOR PANEL FOUND BROKEN AT STA 1715.45 PN 11864182-42 PERFORMED WET LAYUP REPAIR FOR MENTIONED FLOOR PANEL PER SRM 53-00-50-2R, PARGRAPH 3.D, FIG.201 REPAIR MA - [SDR FDEA202204181249](https://openairdocs.org/sdr/FDEA202204181249), Apr 18, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL P.N 11861182-2 FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005.REF ENGINEERING DISPOSITION OF RFTA NO: 02859-0207.P/N: N917FD-N00314-222MEF. B/ - [SDR FDEA202204181248](https://openairdocs.org/sdr/FDEA202204181248), Apr 18, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL NO 221MBF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00309-221MBF. B/N: - [SDR FDEA202204181247](https://openairdocs.org/sdr/FDEA202204181247), Apr 18, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL NO 221AF FOUND WORN REPLACED FLOOR PANEL REP FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00310-221AF. B/N: 20 - [SDR FDEA202204181246](https://openairdocs.org/sdr/FDEA202204181246), Apr 18, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL NO 222AF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005.REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00311-222AF. B/N: 203 All 195: https://openairdocs.org/aircraft/N917FD/reports.md ## STCs that may be installed (OpenAirDocs) (5) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Boeing 757-23A) - [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 757 Series - [STC ST01675CH](https://openairdocs.org/stc/ST01675CH): Installation of Butterfly Valve Ring AIR23028 in starter control valves, part number 775538 or 799700. Cook Airtomic. Lists 757 Series - [STC ST02296AT](https://openairdocs.org/stc/ST02296AT): Upgrade existing HF Voice Communication System to provide HF datalink capability. ARINC, Inc. Lists 757 Series - [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 757 Series - [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 757 Series ## Related - Other Boeing 757-23A aircraft: https://openairdocs.org/model/boeing-757-23a/aircraft.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.